NSN 5340-01-215-6436
Part Details | HELICAL COMPRESSION SPRING SEAT
5340-01-215-6436 A circular item, usually having a flat or grooved flange, boss(es), and/or counterbore designed to accommodate the end of the spring. It is used to position the spring, but does not encase the spring or restrain lateral motion. It may be used in conjunction with a RETAINER, HELICAL COMPRESSION SPRING. Excludes WASHER (1), (as modified); SEAT, BALL SOCKET and HOLDER, SPRING. See also ROTOR, ENGINE POPPET VALVE.
Alternate Parts: 3300819, 3-3008-19, 3300819, 3-3008-19, 5340-01-215-6436, 01-215-6436, 5340012156436, 012156436
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | AUG 28, 1985 | 01-215-6436 | 24328 ( SEAT, HELICAL COMPRESSION SPRING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5340-01-215-6436
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3-3008-19 | 45402 | MEGGITT SAFETY SYSTEMS, INC.DBA MEGGITT CONTROL SYSTEMS-VENTURA |
| 3-3008-19 | 70236 | TACTAIR FLUID CONTROLS, INC. |
Technical Data | NSN 5340-01-215-6436
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225 TO 6, ALLOY 2024 FED SPEC SINGLE MATERIAL RESPONSE |
| SURFACE TREATMENT | ANODIZE |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625, TYPE 2 MIL SPEC SINGLE TREATMENT RESPONSE |
| OVERALL HEIGHT | 0.3750 INCHES NOMINAL |
| END DIAMETER | 0.5450 INCHES NOMINAL |
| DISTANCE FROM END TO FIRST STEP | 0.1750 INCHES NOMINAL |
| FIRST STEP DIAMETER | 0.7400 INCHES NOMINAL |
| FIRST STEP LENGTH | 0.2000 INCHES NOMINAL |
| BORE DIAMETER | 0.5020 INCHES NOMINAL |
| COUNTERBORE DIAMETER | 0.5620 INCHES NOMINAL |
| SEAT ANGLE IN DEG | 45.0 |
| DESIGN TYPE | SOLID |
| FSC APPLICATION DATA | AIRCRAFT HYDRAULIC,VACUUM,DEICING SYSTEMS |